# Service difficulty reports: N452SW

A list on [N452SW](https://openairdocs.org/aircraft/N452SW.md).

Matched to this aircraft by N-number and event date, checked against the reported serial number, make and model. Newest first.

Page 1 of 3 · 110 reports

- [SDR SWIA202162662](https://openairdocs.org/sdr/SWIA202162662.md): None · failed · Nov 19, 2021 · N452SW · Cndair CL6002B19 · Landing Gear Door Actuator
  > D: GEAR DISAGREE WARN MESSAGE UPON PUTTING GEAR DOWN FOR LANDING IN KHOB. QRH PROCEDURE CLEARED MESSAGE. DEN ROAD TRIP MX - DEFERRED LANDING GEAR RETRACTION SYSTEM PER MEL 32-30-1. COMPLIED WITH MAINTENANCE ACTION. INSTALLED PLACARD / C: MEL 32-30-1 / CAT A
- [SDR SWIA2020020748317](https://openairdocs.org/sdr/SWIA2020020748317.md): Rvdt · inoperative · Feb 7, 2020 · N452SW · Cndair CL6002B19 · Landing Gear Steering System
  > STEERING INOP CAUTION MSG IN FLIGHT COMPLIED WITH QRH DID NOT FIX ISSUE. FLIGHT 4449 FILED CLOSEDREMOVED AND REPLACED THE LEFT FEEDBACK RVDT IN REF TO CRJ200 AMM. OPS CHECK GOOD.
- [SDR SWIA2019061445981](https://openairdocs.org/sdr/SWIA2019061445981.md): Skin · chafed · May 17, 2019 · N452SW · Cndair CL6002B19 · Wing, Plate/Skin
  > R/H LWR WING PLANK AND TRAILING EDGE IS CHAFED AT RBL45. (C-CHECK) RO: 06/12/2019 REMOVED CHAFING FROM R/H LWR WING PLANK AND TRAILING EDGE, RBL45 IAW REO AND SRM. PERFORMED PRESSURIZATION CHECK IAW AMM. NO LEAK NOTED
- [SDR SWIA2019061445980](https://openairdocs.org/sdr/SWIA2019061445980.md): Frame · corroded · May 14, 2019 · N452SW · Cndair CL6002B19 · Fuselage Main, Frame
  > FS 333.0 FRAME CORRODED FWD/AFT SIDE FROM STRG 25L TO 26R. (C-CHECK) RO: 06/12/2019 REMOVED AND REPLACED FS333 FRAME ASSY. BETWEEN STR 23L AND STR 23R IAW SRM. / COMPLETED PRESSURE LEAK CHECK IAW AMM. NO LEAKS NOTED.
- [SDR SWIA2019061445979](https://openairdocs.org/sdr/SWIA2019061445979.md): Stringer · corroded · May 14, 2019 · N452SW · Cndair CL6002B19 · Fuselage Main, Longeron/Stringer
  > FS STRG 26L CORRODED FROM FS 319.70 TO FS 349.0. (C-CHECK) RO: 06/12/2019 INSTALLED NEW SPLICE SECTION OF STR 26L FROM FS364 TO FS314 PN: 601R31022-23 AND 2 EACH REPAIR SPLICE CHANNELS PN: N126-7001, AND N126-7606 IAW SRM. COMPLETED PRESSURE LEAK CHECK IAW AM
- [SDR SWIA2019061445978](https://openairdocs.org/sdr/SWIA2019061445978.md): Frame · corroded · May 14, 2019 · N452SW · Cndair CL6002B19 · Fuselage Main, Frame
  > FS 319.70 FRAME CORRODED FWD/AFT SIDE FROM STRG25L TO STRG 26R. (C-CHECK) RO: 06/12/2019 REMOVED AND INSTALLED NEW FS319.70 LOWER FRAME SECTION FROM STR 23L TO STR 23R IAW SRM. COMPLETED PRESSURE LEAK CHECK IAW AMM. NO LEAKS NOTED.
- [SDR SWIA2019061445977](https://openairdocs.org/sdr/SWIA2019061445977.md): Frame · corroded · May 14, 2019 · N452SW · Cndair CL6002B19 · Fuselage Main, Frame
  > FS 310 FRAME FWD/AFT SIDE CORRODED FROM STRG25L TO 26R. (C-CHECK) RO: 06/12/2019 REMOVED AND REPLACED FRAME AT FS310 BETWEEN STR23L TO STR23R IAW SRM. / COMPLETED PRESSURE LEAK CHECK IAW AMM. NO LEAKS NOTED.
- [SDR SWIA2019061445976](https://openairdocs.org/sdr/SWIA2019061445976.md): Strap · corroded · May 13, 2019 · N452SW · Cndair CL6002B19 · Fuselage Miscellaneous Structure
  > RH FLOOR SUPPORT STRAP IS CORRODED AT FS559.00. (C-CHECK) RO: 06/12/2019 REMOVED AND REPLACED WITH NEW FLOOR SUPPORT STRAP P/N 601R31025-29 IAW SRM AND REO. COMPLETED PRESSURE LEAK CHECK IAW AMM. NO LEAKS NOTED.
- [SDR SWIA2019061445975](https://openairdocs.org/sdr/SWIA2019061445975.md): Support · corroded · May 13, 2019 · N452SW · Cndair CL6002B19 · Fuselage Miscellaneous Structure
  > RH SILL AT FS559.00+116 CORRODED. (C-CHECK) RO: 06/12/2019 INSTALLED NEW SILL FROM 559 TO 559+80 IAW SRM.
- [SDR SWIA2019061445974](https://openairdocs.org/sdr/SWIA2019061445974.md): Seat Track · corroded · May 13, 2019 · N452SW · Cndair CL6002B19 · Fuselage, Seat/Cargo Attach Fittings
  > LH SEAT RAIL BEAMS FS559.00+112 TO FS621.00 HAS CORROSION AROUND SCREW HOLES. (C-CHECK) RO: 06/12/2019 REMOVED AND.INSTALLED NEW L/H FLOOR BEAM CAP AT FS 559.00+112 TO FS 621.00 LBL 27 IAW SRM.
- [SDR SWIA2018031944415](https://openairdocs.org/sdr/SWIA2018031944415.md): Proximity Sensor · iced · Mar 19, 2018 · N452SW · Cndair CL6002B19 · Landing Gear Retraction/Extension System
  > NOSE GEAR DISAGREE ON TAKE OFF RETURNED TO FIELD. EMERGENCY WAS DECLARED. PROXIMITY SENSORS WERE COVERED WITH ICE. THAWED ICE FROM GEAR. PERFORMED GEAR SWINGS AND EMERGENCY EXTENSION.
- [SDR SWIA201743311](https://openairdocs.org/sdr/SWIA201743311.md): Floor Support · corroded · Apr 29, 2017 · N452SW · Cndair CL6002B19 · Fuselage Miscellaneous Structure
  > CORROSION ON END FITTING BETWEEN BS 605 TO 621, LBL 27. REPAIRED THE AREA OF THE FLOOR SUPPORT IAW REO.
- [SDR SWIA201743310](https://openairdocs.org/sdr/SWIA201743310.md): Floor Support · corroded · Apr 29, 2017 · N452SW · Cndair CL6002B19 · Fuselage Miscellaneous Structure
  > CORROSION ON END FITTING BETWEEN BS 605 TO 621, LBL 9. REPAIRED THE AREA OF THE FLOOR SUPPORT FITTING IAW REO.
- [SDR SWIA201743309](https://openairdocs.org/sdr/SWIA201743309.md): Floor Support · corroded · Apr 26, 2017 · N452SW · Cndair CL6002B19 · Fuselage Miscellaneous Structure
  > AFT CARGO FLOOR SUPPORT AT LBL 9 BETWEEN BS 589 AND 621 HAS CORROSION AT NUTPLATES. REPAIRED THEFLOOR SUPPORT IAW REO.
- [SDR SWIA201743308](https://openairdocs.org/sdr/SWIA201743308.md): Floor Support · corroded · Apr 26, 2017 · N452SW · Cndair CL6002B19 · Fuselage Miscellaneous Structure
  > AFT CARGO FLOOR SUPPORT AT LBL 27 BS 605 TO 621 HAS CORROSION AT NUTPLATES. REPAIRED THE FLOOR SUPPORT IAW REO.
- [SDR SWIA201743307](https://openairdocs.org/sdr/SWIA201743307.md): Door Sill · corroded · Apr 26, 2017 · N452SW · Cndair CL6002B19 · Fuselage Miscellaneous Structure
  > AFT CARGO DOOR SILL HAS CORROSION AT NUTPLATES. REPAIRED THE DOOR SILL IAW REO.
- [SDR SWIA201743306](https://openairdocs.org/sdr/SWIA201743306.md): Skin · chafed · Apr 25, 2017 · N452SW · Cndair CL6002B19 · Ailerons
  > PANEL 699CB HAS CHAFED. REPAIRED THE RT AILERON SHROUD PANEL IAW REO.
- [SDR SWIA201743305](https://openairdocs.org/sdr/SWIA201743305.md): Skin · chafed · Apr 25, 2017 · N452SW · Cndair CL6002B19 · Ailerons
  > PANEL 699BB HAS MULTIPLE CHAFE SPOTS. REPAIRED THE AILERON LOWER SKIN PANEL IAW REO.
- [SDR SWIA201743304](https://openairdocs.org/sdr/SWIA201743304.md): Skin · chafed · Apr 25, 2017 · N452SW · Cndair CL6002B19 · Ailerons
  > RIGHT AILERON, LOWER SHROUD PANEL 699AB IS CHAFED. REPAIRED THE AILERON LOWER SKIN IAW REO.
- [SDR SWIA201743303](https://openairdocs.org/sdr/SWIA201743303.md): Vane · chafed · Apr 24, 2017 · N452SW · Cndair CL6002B19 · Trailing Edge Flaps
  > LEFT INBOARD FLAP VANE, THE OTBD LEADING EDGE IS CHAFED. REMOVED AND REPLACED THE FLAP VANE IAW SRM.
- [SDR SWIA201743302](https://openairdocs.org/sdr/SWIA201743302.md): Vane · chafed · Apr 24, 2017 · N452SW · Cndair CL6002B19 · Trailing Edge Flaps
  > LEFT INBOARD FLAP VANE, THE MID-CENTER LEADING EDGE IS CHAFED. REPLACED THE FLAP VANE CAP IAW SRM.
- [SDR SWIA201541105](https://openairdocs.org/sdr/SWIA201541105.md): Support Bracket · cracked · Apr 20, 2015 · N452SW · Cndair CL6002B19 · Fuselage Miscellaneous Structure
  > RT SIDE WHEEL WELL HAS HYDRAULIC LINES SUPPORT BRACKET CRACK NEXT. BRAKE APPLICATION PRESSURE TRANSDUCER C-CHECK, RO 4/22/15. INSTALLED SERVICEABLE RH WHEEL WELL HYD. LINES SUPPORT BRACKET NEXT TO BRAKE APPLICATION PRESSURE TRANSDUCER REF STS EA.
- [SDR SWIA201541101](https://openairdocs.org/sdr/SWIA201541101.md): Support Bracket · cracked · Apr 20, 2015 · N452SW · Cndair CL6002B19 · Fuselage Miscellaneous Structure
  > LEFT SIDE WHEEL WELL HAS BRAKE APPLICATION PRESSURE TRANSDUCER SUPPORT BRACKET CRACK. C-CHECK RO 4/22/15, REMOVED DAMAGED LT WHEEL WELL BRAKE APPLICATION PRESSURE TRANSDUCER SUPPORT BRACKET AND REPLACED WITH SERVICEABLE BRACKET REF STS EA.
- [SDR SWIA201541100](https://openairdocs.org/sdr/SWIA201541100.md): Support Bracket · cracked · Apr 20, 2015 · N452SW · Cndair CL6002B19 · Fuselage Miscellaneous Structure
  > LT SIDE WHEEL WELL HAS VOLUMETRIC FUSE SUPPORT BRACKET CRACK. C-CHECK, RO 4/22/15, REMOVED DAMAGED LT SIDE VOLUMETRIC FUSE SUPPORT BRACKET AND REPLACED WITH SERVICEABLE BRACKET REF STS EA.
- [SDR SWIA201541095](https://openairdocs.org/sdr/SWIA201541095.md): Support Bracket · cracked · Apr 20, 2015 · N452SW · Cndair CL6002B19 · Fuselage Miscellaneous Structure
  > RT SIDE WHEEL WELL HAS BRAKE APPLICATION PRESSURE TRANSDUCER SUPPORT BRACKET CRACK. C-CHECK, COMPLIED WITH STS EA, REMOVED DAMAGED RT WHEEL WELL BRAKE APPLICATION PRESSURE TRANSDUCER SUPPORT BRACKET AND REPLACED WITH SERVICEABLE BRACKET REF STS EA,
- [SDR SWIA201541094](https://openairdocs.org/sdr/SWIA201541094.md): Support Bracket · cracked · Apr 20, 2015 · N452SW · Cndair CL6002B19 · Fuselage Miscellaneous Structure
  > RIGHT SIDE WHEEL WELL HAS VOLUMETRIC FUSE SUPPORT BRACKET CRACK. C-CHECK, COMPLIED WITH STS EA. REMOVED DAMAGED RT SIDE VOLUMETRIC FUSE SUPPORT BRACKET AND REPLACED WITH SERVICEABLE BRACKET.
- [SDR SWIA201541109](https://openairdocs.org/sdr/SWIA201541109.md): Post · cracked · Apr 7, 2015 · N452SW · Cndair CL6002B19 · Fuselage Miscellaneous Structure
  > FS409 +128, LBL18 POST HAS CRACK AT BOTTOM SIDE, MARKED, C-CHECK, RO 4/22/15, INSTALLED INBD AND OTBD VERTICAL POSTS AT FS 409+128, LBL 18, REF REO.
- [SDR SWIA201541108](https://openairdocs.org/sdr/SWIA201541108.md): Post · cracked · Apr 7, 2015 · N452SW · Cndair CL6002B19 · Fuselage Miscellaneous Structure
  > FS409 +128 LBL27 POST HAS POSSIBLE CRACK EVALUATED AT BOTTOM SIDE, MARKED, C-CHECK RO 4/22/15. INSTALLED VERTICAL POST AT FS 409+128, LBL 27, INBD SIDE REF SRM & STS EA.
- [SDR SWIA201541107](https://openairdocs.org/sdr/SWIA201541107.md): Post · cracked · Apr 7, 2015 · N452SW · Cndair CL6002B19 · Fuselage Miscellaneous Structure
  > FS409 +128, RBL18 POST HAS POSSIBLE CRACK EVALUATE AT BOTTOM SIDE, MARKED OTBD SIDE. C-CHECK RO 4/22/15, LOCATED AND DRILLED NEW POST AT FS.409, RBL.18 OTBD SIDE REF AND REO.
- [SDR SWIA201541106](https://openairdocs.org/sdr/SWIA201541106.md): Post · cracked · Apr 7, 2015 · N452SW · Cndair CL6002B19 · Fuselage Miscellaneous Structure
  > FS409 +128 RBL27, POST HAS POSSIBLE CRACK EVALUATE AT BOTTOM SIDE, MARKED INBD SIDE. C-CHECK RO 4/22/15, LOCATED, FIT AND DRILLED NEW VERTICAL POST AT FS 409+128, RBL 27 INBD REF SRM INSTALLED NEW VERT POST AT FS 409, RBL 27 INBD SECTION SRM 51 AND STS EA.
- [SDR SWIA201541104](https://openairdocs.org/sdr/SWIA201541104.md): Floorbeam · cracked · Apr 6, 2015 · N452SW · Cndair CL6002B19 · Fuselage Main, Floor Beam
  > CRACK AT FS 280.00 BEAM WEB AT RBL 9, C-CHECK RO 4/22/15, COMPLIED REPAIR OF THE FS 280.00 BEAM WEB AT RBL 9, REF REO.
- [SDR SWIA201541099](https://openairdocs.org/sdr/SWIA201541099.md): Floor Panel · cracked · Apr 6, 2015 · N452SW · Cndair CL6002B19 · Fuselage Floor Panel
  > PRESSURE FLOOR SKIN PANEL CRACK AT FS460.00 BETWEEN BL0.0 AND LBL9.0, C-CHECK, RO 4/22/15. INSTALLED REPAIR DOUBLERS: -3, -5, -7, -9, REF REO.
- [SDR SWIA201541098](https://openairdocs.org/sdr/SWIA201541098.md): Vane · failed · Apr 5, 2015 · N452SW · Cndair CL6002B19 · Trailing Edge Flaps
  > RT INBD FLAP VANE CENTER L/E SECTION WORN OUT OF LIMITS REPLACE, C-CHECK RO 4/22/15, R & R BAD RT INBD FLAP VANE L/E SECTION WITH NEW PART REF DWG 601R14303, REV J, DATED MAY/13, 1996. RESTORED FINISH REF STS E/A.
- [SDR SWIA201541097](https://openairdocs.org/sdr/SWIA201541097.md): Vane · chafed · Apr 4, 2015 · N452SW · Cndair CL6002B19 · Trailing Edge Flaps
  > RIGHT INBD FLAP VANE L/E CHAFED, OTBD OF CENTER VANE MOUNT. C-CHECK RO 4/22/15, EVALUATED CHAFE MARK RT INBD FLAP VANE CENTER L/E SECTION ORIGINAL MATERIAL THICKNESS IS 0.050 REMAINING MATERIAL 0.000 FLAP VANE CENTER SECTION IS OUT OF REPAIRABLE LIMITS REF RE
- [SDR SWIA201541096](https://openairdocs.org/sdr/SWIA201541096.md): Structure · chafed · Apr 4, 2015 · N452SW · Cndair CL6002B19 · Landing Gear Doors
  > RT MLG DOOR AFT OTBD EDGE CHAFED. C-CHECK, RO 4/22/15, COMPLIED WITH REPAIR OF RT MLG DOOR OTBD EDGE REF REO.
- [SDR SWIA201541103](https://openairdocs.org/sdr/SWIA201541103.md): Skin · dented · Apr 3, 2015 · N452SW · Cndair CL6002B19 · Fuselage Main, Plate/Skin
  > DENT BELOW CARGO DOOR JUST AFT OF FRAME FS605 AND JUST ABOVE STRINGER 22L. C-CHECK, RO 4/22/15, INSTALLED REPAIR PARTS TO OUTER SKIN AT FRAME FS 605.0 AND STR 22L, REF STS EA.
- [SDR SWIA201541102](https://openairdocs.org/sdr/SWIA201541102.md): Skin · dented · Apr 3, 2015 · N452SW · Cndair CL6002B19 · Wing, Plate/Skin
  > FOUND A DENT ON THE RT UPPER WING SURFACE 5.25" OTBD OF WS 47.61, 11.25" FORWARD OF THE WING T/E AND 2.5" INBD OF THE RT WING INBD GROUND SPOILER. DENT DEPTH IS 0.0255". PERMANENT REPAIR, COMPLETED ON RH UPPER WING SURFACE 5.25" OTBD OF WS 47.61, 11.25" FORW
- [SDR SWIA201440423](https://openairdocs.org/sdr/SWIA201440423.md): Mount · galled · Dec 19, 2014 · N452SW · Cndair CL6002B19 · Engine Mount Section
  > RT ENGINE FORWARD MOUNT LINK ASSY AND CLAMP BUSHING GALLED. R & R RT FWD MOUNT LINK ASSY IAW AMM.
- [SDR SWIA201439031](https://openairdocs.org/sdr/SWIA201439031.md): Battery Pack · failed · Aug 9, 2014 · N452SW · Cndair CL6002B19 · Emergency Lighting
  > EMERGENCY LIGHTS DO NOT COME. R & R ALL FOUR BATTERY PACKS IAW AMM. OPS CHECKED GOOD.
- [SDR SWIA201436586](https://openairdocs.org/sdr/SWIA201436586.md): Strip · rough · Mar 2, 2014 · N452SW · Cndair CL6002B19 · Trailing Edge Flaps
  > WHEN SELECTING FLAPS 45, AIRCRAFT HAS PROMINENT RIGHT ROLL CHARACTERISTICS THAT NEEDS ALMOST 1/2 OF THE LT AILERON TRIM TO NEUTRALIZE. FLT 4689 SANDED RT OTBD FLAP TEFLON STRIP LE TO A SMOOTH TRANSITION TO THE ADJACENT PAINT SURFACE IAW AMM.
- [SDR SWIA201334723](https://openairdocs.org/sdr/SWIA201334723.md): Light · inoperative · Sep 23, 2013 · N452SW · Cndair CL6002B19 · Emergency Lighting
  > 1ST EMERGENCY OVERHEAD LIGHT IS OUT. FLT#4830 RELAMPED.
- [SDR SWIA201333366](https://openairdocs.org/sdr/SWIA201333366.md): Lever · chafed · Apr 18, 2013 · N452SW · Cndair CL6002B19 · Passenger/Crew Doors
  > MAIN CABIN DOOR FORWARD PULL-IN LEVER IS CHAFED. (C-CHECK) MAIN CABIN DOOR FORWARD PULL-IN LEVER REPAIRED IAW REO.
- [SDR SWIA201333367](https://openairdocs.org/sdr/SWIA201333367.md): Post · cracked · Apr 15, 2013 · N452SW · Cndair CL6002B19 · Fuselage Miscellaneous Structure
  > FS 409.0+128 RBL 18.00 INBD AFT RADIUS OF VERT POST CRACK INDICATION NOTED. (C-CHECK) REPLACED CRACKED POST WITH NEW POST AT FS 409+ 128 IAW REO.
- [SDR SWIA201332864](https://openairdocs.org/sdr/SWIA201332864.md): Controller · failed · Feb 22, 2013 · N452SW · Cndair CL6002B19 · Cabin Pressure Controller
  > NO PRESSURIZATION, SWITCHED TO MANUAL MODE FOR REMAINDER OF THE FLIGHT. (FLT 4713) REPLACED NR 1 PRESSURE CONTROLLER AND CABIN PRESS CONTROL PANEL ASSEMBLY IAW AMM. OPS CHECK NORMAL. P/N: 2119768-8 S/N ON: 61-C1162 S/N OFF: 92-C1480 P/N: 2119764-6 S/N ON
- [SDR SWIA201332784](https://openairdocs.org/sdr/SWIA201332784.md): Inverter · inoperative · Feb 8, 2013 · N452SW · Cndair CL6002B19 · Emergency Lighting
  > RIGHT SIDE NR 3 LOWER EMERGENCY EXIT SIGN DOES NOT ILLUMINATE. (FLT 4719) REPLACED NR 3 EMERGENCY LIGHT INVERTER.
- [SDR SWIA201232439](https://openairdocs.org/sdr/SWIA201232439.md): Light · inoperative · Dec 23, 2012 · N452SW · Cndair CL6002B19 · Emergency Lighting
  > NR 2 EMERGENCY OVERHEAD LIGHT BURNED OUT. (FLT 4754) RELAMPED EMERGENCY LIGHT.
- [SDR SWIA201232256](https://openairdocs.org/sdr/SWIA201232256.md): Light · inoperative · Nov 28, 2012 · N452SW · Cndair CL6002B19 · Emergency Lighting
  > EMERGENCY SIGN AT EXIT ROW RT SIDE BURNED OUT. (FLT 4716) RELAMPED EMERGENCY SIGN.
- [SDR SWIA201232143](https://openairdocs.org/sdr/SWIA201232143.md): Connector · loose · Nov 9, 2012 · N452SW · Cndair CL6002B19 · Light System Wiring
  > LOWER EMERGENCY EXIT SIGN AT SEAT 8D IS OUT. (FLT 4517) RE-SECURED LOOSE CONNECTION ON LOWER EMERGENCY EXIT SIGN ON ROW 8D.
- [SDR SWIA201232041](https://openairdocs.org/sdr/SWIA201232041.md): Battery Pack · discharged · Oct 26, 2012 · N452SW · Cndair CL6002B19 · Emergency Lighting
  > RIGHT SIDE OVERWING EXIT LOWER BLUE LIGHT IS INOPERATIVE. (FLT 4514) REPLACED NR 4 EMERGENCY LIGHTING BATTERY PACK IN REFERENCE TO AMM. P/N: AD-2013-1A S/N OFF: 72169.
- [SDR SWIA201231542](https://openairdocs.org/sdr/SWIA201231542.md): Light · inoperative · Aug 15, 2012 · N452SW · Cndair CL6002B19 · Emergency Lighting
  > NR 5 OVERHEAD EMERGENCY LIGHT IS OUT. (SERVICE) RELAMPED EMERGENCY LIGHT.

Next page: https://openairdocs.org/aircraft/N452SW/reports.md?page=2

## The whole list in SQL

Runs in DuckDB 1.2 or later on the release's Parquet files over HTTPS:

```sql
SELECT sdr_id, difficulty_date, n_number, aircraft_make, aircraft_model, part_name, part_condition, jasc_code, discrepancy
FROM 'https://openairdocs.org/data/latest/faa_service_difficulty_report.parquet'
WHERE n_number = 'N452SW' AND registry_match = 'registration'
ORDER BY difficulty_date DESC
```

This list as a web page: https://openairdocs.org/aircraft/N452SW/reports

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